Classifications

• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
  • C21D8/0273—Final recrystallisation annealing
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
  • C21D1/18—Hardening; Quenching with or without subsequent tempering
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D6/00—Heat treatment of ferrous alloys
  • C21D6/002—Heat treatment of ferrous alloys containing Cr
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D6/00—Heat treatment of ferrous alloys
  • C21D6/005—Heat treatment of ferrous alloys containing Mn
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D6/00—Heat treatment of ferrous alloys
  • C21D6/008—Heat treatment of ferrous alloys containing Si
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
  • C21D8/0226—Hot rolling
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
  • C21D8/0236—Cold rolling
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
  • C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
  • C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D2211/00—Microstructure comprising significant phases
  • C21D2211/001—Austenite
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D2211/00—Microstructure comprising significant phases
  • C21D2211/005—Ferrite
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D2211/00—Microstructure comprising significant phases
  • C21D2211/008—Martensite

Definitions

• the present invention relates to high strength steel sheets suitable for applications in automobiles.
• the invention relates to cold rolled steel sheets having a tensile strength of at least 980 MPa and having excellent global formability and excellent bending property.
• Automotive body parts are often stamped out of sheet steels, forming complex structural members of thin sheet.
• such parts cannot be produced from conventional high strength steels, because of a too low formability for complex structural parts.
• multiphase Transformation Induced Plasticity aided steels TRIP steels
• TRIP steels have gained considerable interest in the last years, in particular for use in auto body structural parts.
• TRIP steels possess a multi-phase microstructure, which includes a meta-stable retained austenite phase, which is capable of producing the TRIP effect.
• austenite transforms into martensite, which results in remarkable work hardening.
• This hardening effect acts to resist necking in the material and postpone failure in sheet forming operations.
• the microstructure of a TRIP steel can greatly alter its mechanical properties.
• W02018/09090 A1 discloses a high strength TBF steel with a high yield ratio (local formability) with excellent resistance to edge cracking and a high hole expansion ratio. Although these steels disclose several attractive properties there is demand for 980 MPa steel sheets having an improved property profile with respect global formability and bending properties. Particularly, the B-pillar hinge, roof rail, door panel or similar parts of an automobile would have use of such material.
• the present invention is directed to high strength (TBF) steel sheets having a tensile strength of 980 - 1180 MPa and an excellent global formability and excellent bending properties. It should further be possible to produce the steel sheets on an industrial scale in a Continuous Annealing Line (CAL).
• CAL Continuous Annealing Line
• the invention aims at providing a steel composition that can be processed to complicated structural members, where both yield ratio, which affect the global formability, and bendability is of importance. It is particularly suitable for a B-pillar hinge, roof rail, door panel or similar parts in an automobile.
• Fig. l is a diagram where the bendability Ri/t is plotted against the yield ratio.
• the steel sheet has a composition consisting of the following alloying elements (in wt.
• C stabilizes the austenite and is important for obtaining sufficient carbon within the retained austenite phase.
• C is also important for obtaining the desired strength level. Generally, an increase of the tensile strength in the order of 100 MPa per 0.1 %C can be expected. When C is lower than 0.08 % then it is difficult to attain a tensile strength of 980 MPa. If C exceeds 0.14 %, then the weldability is impaired.
• the upper limit may be 0.13 or 0.12 %.
• the lower limit may be 0.09, or 0.10 %.
• a preferred range is 0.09 - 0.12 %.
• Mn 2.5 - 3.0 %
• Manganese is a solid solution strengthening element, which stabilises the austenite by lowering the M s temperature and prevents ferrite and pearlite to be formed during cooling.
• Mn lowers the A C 3 temperature and is important for the austenite stability.
• a tensile strength of 980 MPa and the austenitizing temperature might be too high for conventional industrial annealing lines.
• at lower contents it may be difficult to avoid the formation of polygonal ferrite.
• the upper limit may therefore be 3.0, 2.9, 2.8 or 2.7 %.
• the lower limit may be 2.5, or 2.6 %.
• Si acts as a solid solution strengthening element and is important for securing the strength of the thin steel sheet. Si suppresses the cementite precipitation and is essential for austenite stabilization. However, if the content is too high, then to much silicon oxides will form on the strip surface, which may lead to cladding on the rolls in the CAL and surface defects on subsequently produced steel sheets.
• the upper limit is therefore 1.1 % and may be restricted to 1.05, 1.0 or 0.95 %.
• the lower limit may be 0.75 or 0.80 %.
• a preferred range is 0.7 - 1.0 %.
• Cr is effective in increasing the strength of the steel sheet. Cr is an element that forms ferrite and retards the formation of pearlite and bainite. The A C 3 temperature and the M s temperature are only slightly lowered with increasing Cr content. Cr results in an increased amount of stabilized retained austenite.
• the amount of Cr is limited to 0.4 %. The upper limit may be 0.35, 0.30 or 0.25 %. The lower limit may be 0.10, or 0.15 %. A preferred range is 0.1 - 0.3 %.
• A1 promotes ferrite formation and is also commonly used as a deoxidizer.
• the M s temperature is increased with an increasing Al content.
• a further drawback of Al is that it results in a drastic increase in the A C 3 temperature and therefore makes it more difficult to austenitize the steel in the CAL.
• the Al content is preferably limited to less than 0.2 %, more preferably to less than 0.1 %, most preferably less than 0.06 %.
• Nb ⁇ 0.1 %
• Nb is commonly used in low alloyed steels for improving strength and toughness, because of its influence on the grain size. Nb increases the strength elongation balance by refining the matrix microstructure and the retained austenite phase due to precipitation of NbC.
• the steel may contain Nb in an amount of ⁇ 0.1 %. A deliberate addition of Nb is not necessary according to the present invention.
• the upper limit may therefore be restricted to ⁇ 0.03 %.
• the upper limit may further be restricted to 0.01, or 0.005 %.
• Molybdenum can be added to improve strength. It may further enhance the benefits of NbC precipitates by reducing the carbide coarsening kinetics. A deliberate addition of Mo is not necessary according to the present invention.
• the upper limit may therefore be restricted to ⁇ 0.03 %.
• the upper limit may further be restricted to 0.02, or 0.01 %.
• V ⁇ 0.1%
• the function of V is similar to that of Nb in that it contributes to precipitation hardening and grain refinement.
• the steel may contain V in an amount of ⁇ 0.1 %.
• the upper limit may be restricted to 0.09, 0.07, 0.05, 0.03, or 0.01 %.
• a deliberate addition of V is not necessary according to the present invention. The upper limit may therefore be restricted to ⁇ 0.01 %.
• Ti is commonly used in low alloyed steels for improving strength and toughness, because of its influence on the grain size by forming carbides, nitrides or carbonitrides.
• Ti is a strong nitride former and can be used to bind the nitrogen in the steel.
• the upper limit may be restricted to 0.09, 0.07, 0.05, 0.03, or 0.01 %.
• a deliberate addition of Ti is not necessary according to the present invention. The upper limit may therefore be restricted to ⁇ 0.005%.
• Ca ⁇ 0.05 Ca may be used for the modification of the non-metallic inclusions.
• the upper limit is 0.05% and may be set to 0.04, 0.03, 0.01 %.
• a deliberate addition of Ca is not necessary according to the present invention.
• the upper limit may therefore be restricted to ⁇ 0.004%.
• Cu is an undesired impurity element that is restricted to ⁇ 0.1 % by careful selection of the scrap used.
• the upper limit may be restricted to ⁇ 0.06%.
• Ni is an undesired impurity element that is restricted to ⁇ 0.2 % by careful selection of the scrap used.
• the upper limit may be restricted to ⁇ 0.08%.
• B is an undesired impurity element that is restricted to ⁇ 0.005 % by careful selection of the scrap used. B increases hardness but may come at a cost of reduced bendability and is therefore not desirable in the present suggested steel. B may further make scrap recycling more difficult and an addition of B may also deteriorate workability. A deliberate addition of B is therefore not desired according to the present invention. The upper limit may therefore be restricted to ⁇ 0.0006%.
• N ⁇ 0.015 %, preferably 0.003 - 0.008 %
• Oxygen and hydrogen can further be limited to O: ⁇ 0.0003 H: ⁇ 0.0020
• the high strength TRIP-assisted bainitic ferrite (TBF) steel sheets of the present invention have microstructure mainly consisting of retained austenite inclusions embedded in the matrix.
• microstructural constituents are in the following expressed in volume % (vol. %).
• the steel comprises a matrix of bainitic ferrite (BF). Hence, the amount of bainitic ferrite is generally > 50 %.
• the microstructure may also contain tempered martensite (TM). The constituents BF and TM may be difficult to distinguish from each other.
• the total content of both constituents may be limited to 70 - 90 %.
• the amount is normally in the range of 75 - 85 %.
• Martensite may be present in the final microstructure because, depending on its stability, some austenite may transform to martensite during cooling at the end of the overaging step. Martensite may be present in an amount of ⁇ 15 %, preferably ⁇ 10 %. The amount is normally in the range of 5 - 10%. These un-tempered martensite particles are often in close contact with the retained austenite particles, and they are therefore often referred to as martensite-austenite (MA) particles.
• MA martensite-austenite
• Retained austenite is a prerequisite for obtaining the desired TRIP effect.
• the amount of retained austenite should therefore be in the range of 2 - 20 %, preferably 5 - 15 %.
• the amount of retained austenite was measured by means of the saturation magnetization method described in detail in Proc. Int. Conf. on TRIP-aided high strength ferrous alloys (2002), Ghent, Belgium, p. 61-64.
• Polygonal ferrite (PF) is not a desired microstructural constituent and is therefore limited to ⁇ 10 %, preferably ⁇ 5 %, ⁇ 3 % or ⁇ 1 %. Most preferably, the steel is free from PF.
• the mechanical properties of the claimed steel are important and at least one of the following requirements should be fulfilled: tensile strength (R m ) 980 - 1180 MPa yield strength (Rpo .2 ) 580 - 750 MPa total elongation (A 50 ) > 11% yield ratio (Rpo .2 / Rm) ⁇ 0.72 bendability (Ri/t) ⁇ 2
• the upper limit of the tensile strength (R m ) can further be limited to 1160, 1140, 1120, or 1100 MPa.
• the lower limit may further be limited to 990 or 1000 MPa.
• the upper limit of the yield strength (Rpo . 2) can further be limited to 740, 730, 720, 710, 700, 890, 680, 670, or 660 MPa.
• a preferred interval is 580-700 MPa.
• the upper limit of the yield ratio (Rpo . 2/ Rm) can further be limited to 0.71, 0.70, 0.69, 0.68, 0.67, 0.66, or 0.65.
• the lower limit could be 0.50, 0.51, 0.52, 0.53, 0.54, 0.55, 0.56, 0.57 or 0.58.
• the Rm, Rpo .2 values as well as the total elongation (A50) are derived in accordance with the Japanese Industrial Standard JIS Z 2241 : 2011, wherein the samples are taken in the transversal direction of the strip.
• the upper limit of the bendability Ri/t may further be limited to 1.9, 1.8, 1.7, 1.6 or 1.5. Preferably Ri/t ⁇ 1.7, more preferably ⁇ 1.5.
• the lower limit of Ri/t may be 0.5, 0.6, 0.7, 0.8, 0.9, or 1.0.
• the bendability is evaluated by the ratio of the limiting bending radius (Ri), which is defined as the minimum bending radius with no occurrence of cracks, and the sheet thickness, (t).
• a 90° V-shaped block is used to bend the steel sheet in accordance with JIS Z2248.
• the sample size is 35x100 mm.
• the bending value Ri/t is obtained by dividing the limit bending radius in mm with the thickness in mm.
• the mechanical properties of the steel sheets of the present invention can be largely adjusted by the alloying composition and the microstructure.
• the microstructure can be adjusted by the heat treatment in the CAL, in particular by the isothermal treatment temperature in the overaging step.
• the suggested steel can be produced by making steel slabs of the conventional metallurgy by converter melting and secondary metallurgy with the composition suggested above.
• the slabs are hot rolled in austenitic range to a hot rolled strip.
• the hot rolled strip is coiled at a coiling temperature in the range of 500 - 650 °C.
• a scale removal process such as pickling.
• the coiled strip is thereafter batch annealed at a temperature in the range of 500 - 650 °C, preferably 550 - 650 °C, for a duration of 5 - 30h. Thereafter cold rolling the annealed steel strip with a reduction rate between 35 and 90%, preferably around 40 - 60% reduction. Further treating the cold rolled steel strip in a Continuously Annealing Line (CAL).
• CAL Continuously Annealing Line
• the annealing cycle in the CAL includes heating to a temperature of 800 - 890 °C, preferably 840-860 °C, soaking for 80-180 s, preferably 100- 140s, slow gas jet cooling at a rate of 5-15 °C/s to a temperature of 700-750 °C, rapid gas cooling at a rate of 20 - 60 °C/s, preferably 30 - 50 °C/s to an overaging temperature of 405 - 460 °C, holding for 150 to 1000 s, before cooling to room temperature.
• the overaging temperature may be upward limited to 450, 440, 430 or 420 °C.
• the lower limit may be 405, 406, 407, 408, 409, or 410 °C.
• a preferred range for the overaging temperature is 405 - 420 °C.
• Steels 11-13, and reference steels R1-R3 were produced by conventional metallurgy by converter melting and secondary metallurgy.
• the compositions are shown in table 1, further elements were present only as impurities, and below the lowest levels specified in the present description.
• Table 1 disclose the composition of the examined steel sheets.
• Table 1 Composition of examined steel sheets. Slabs of the steel alloys were produced in a continuous caster. The slabs were reheated and subjected to hot rolling to a thickness shown in table 2. The hot rolling finishing temperature was about 900 °C and the coiling temperature about 550 °C. The hot rolled strips were pickled and batch annealed at about 620-625 °C for a time of 10 hours in order to reduce the tensile strength of the hot rolled strip and thereby reducing the cold rolling forces. The strips were thereafter cold rolled in a five stand cold rolling mill to a final thickness of about 1.4 mm (II, 13, Rl, R2) or 1 mm (12, R3) and finally subjected to continuous annealing.
• Table 1 Composition of examined steel sheets.
• Table 2 discloses the hot and cold rolling parameters. The batch annealing was performed between the hot- and cold rolling steps for about 10 h.
• the annealing cycle consisted of heating to a temperature of about 850 °C, soaking for about 120 s, slow gas jet cooling at a rate of about 10 °C/s to a temperature of about 720 °C, rapid gas cooling at a rate of about 40 °C/s to an overaging temperature of above 405 °C for the inventive examples, and about 390 - 395 °C for the non-inventive examples, isothermal holding at the overaging temperature and final cooling to ambient temperature.
• the inventive steels 11-13 has a yield strength below 750 MPa.
• all inventive examples disclose a bendability (Ri/t) less than 2.0 in combination with a yield ratio of less than 0.72.
• the highest Ri/t was 1.5 .and the highest yield ratio was 0.64.
• the reference steels R1-R3 do not meet the requirements of yield strength, and yield ratio in combination with bendability.
• Fig. l is a diagram where the bendability Ri/t is plotted against the yield ratio.
• the examples 11-13 are within the claimed border of claim 1, marked as “area of protection”, whereas the refence R1-R3 are outside of it.
• the R m and R p o , 2 values are derived according to the European norm EN 10002 Part 1, wherein the samples were taken in the longitudinal direction of the strip.
• the elongation (A50) is derived in accordance with the Japanese Industrial Standard JIS Z 2241 : 2011 for samples taken in the transversal direction of the strip.
• Ri/t was determined in V bend test in accordance with JIS Z2248. Samples (35x100 mm) of the produced strips were subjected to the Y bend test to find out the limiting bending radius (Ri). The samples were examined both by eye and under optical microscope with 25 times magnification in order to investigate the occurrence of cracks. Ri/t was determined by dividing the limiting bending radius (Ri) with the thickness of the cold rolled strip (t). Ri is the largest radius in which the material shows no cracks after three bending tests.
• the material of the present invention can be widely applied to high strength structural parts in automobiles.
• the high strength steel sheets are particularly well suited for the production of parts having high demands global formability and bendability. It is particularly suitable for a B-pillar hinge, roof rail or door panel of an automobile..

Landscapes

• Chemical & Material Sciences (AREA)
• Engineering & Computer Science (AREA)
• Materials Engineering (AREA)
• Mechanical Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• Physics & Mathematics (AREA)
• Thermal Sciences (AREA)
• Crystallography & Structural Chemistry (AREA)
• Heat Treatment Of Sheet Steel (AREA)

Applications Claiming Priority (2)

Publications (1)

Family

ID=81308219

Family Applications (1)

Country Status (7)

Family Cites Families (11)

• 2021
  • 2021-04-07 SE SE2150431A patent/SE544819C2/en unknown
• 2022
  • 2022-04-05 JP JP2023561357A patent/JP2024513104A/ja active Pending
  • 2022-04-05 CN CN202280026011.XA patent/CN117480271A/zh active Pending
  • 2022-04-05 WO PCT/EP2022/059016 patent/WO2022214488A1/en active Application Filing
  • 2022-04-05 US US18/283,961 patent/US20240167137A1/en active Pending
  • 2022-04-05 KR KR1020237036779A patent/KR20240019756A/ko unknown
  • 2022-04-05 EP EP22716432.4A patent/EP4320281A1/en active Pending

Also Published As

Similar Documents

Legal Events